I am simulating a duct with rectangular section without heat transfer and laminar flow. All of all are abdiabatic.

I m doing a study of indenpende of mesh but the results not converge. What can I be doing wrong? The problem is very simple.

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hugo CFD
posted this
13 June 2018
- Last edited 13 June 2018

I am simulating a duct with rectangular section without heat transfer and laminar flow. All of all are abdiabatic.

I m doing a study of indenpende of mesh but the results not converge. What can I be doing wrong? The problem is very simple.

Kremella
posted this
15 June 2018

Hello hugo CFD,

Are you saying your results are not grid independent? If so, could you please post some snapshots of the grid? Also, please elaborate on how you are conducting this study.

Thank you.

Best Regards,

Karthik

hugo CFD
posted this
15 June 2018
- Last edited 15 June 2018

yes. I used the grid that you can see in the pictures. This mesh represents the most refined mesh.

I am analyzing a duct with the following dimensions.

Cross section : length- 9mm; witdh- 4mm

and length total 500 mm.

The skewness is less than 0,65 for all of grids.

I am analyzing a quarter of the duct.

The first mesh I used has the following characteristics:

size element: 0,7 mm,

Inflation: layer 7; total thickness: 0,3 mm

Then I studied the 3 most refined meshes with a ratio of 1.4 relative to the element size and number of layers used in the inflation. I got the following results for the average pressure throughout the duct.

0,7 mm; 7 layers - 4,539; 0,5 mm; 10 layers - 4,603; 0,357 mm; 14 layers - 4,638; 0,255 mm; 19 layers - 4,664;

thank you

hugo

raul.raghav
posted this
15 June 2018

Hugo, you're doing a laminar flow problem. There is no point in increasing the number of inflation layers beyond a certain point. Just focus on increasing the element size. I'd recommend a ratio of 2 for the element size. Say, for e.g., 1mm, 0.5mm, 0.25mm, 0.125mm...

And you are achieving convergence from your study if you notice it. I hope you're reporting the pressure drop across the duct. Based on those values, you're error is down to less than 0.5%. That's good for grid convergence study.

Rahul

hugo CFD
posted this
17 June 2018
- Last edited 18 June 2018

Oi.

Why did you recommend ratio 2?

Hugo

raul.raghav
posted this
18 June 2018

The mesh refinement depends on the geometry and the physics of the problem. So a standard ratio for grid independence doesn't have to be a certain number. The whole idea is to have a * coarse*,

Rahul

hugo CFD
posted this
18 June 2018

Another question.

why should I not increase the refinement of inflation, only the dimensions of the element?

Hugo

Kremella
posted this
19 June 2018

Since you are solving a laminar flow, refining your inflation layers might not matter 'beyond a certain point' (as pointed out by Rahul). As long as you have a 'sufficiently' fine inflation grid to resolve your boundary layer gradients, you should be set. Now, what is sufficiently 'fine' is something you will have to experiment with and figure out for yourself. This exercise again is similar to your initial grid refinement question.

raul.raghav
posted this
19 June 2018
- Last edited 19 June 2018

As Karthik mentioned, sufficiently 'fine' is based on your judgement. You define the total thickness of your inflation layers to be 0.3mm and adding 15 or 20 inflation layers is not going to make a huge difference particularly for low Re flows. What you're doing is absolutely right and that is the correct way of doing grid convergence study, however, depending on the physics of your problem, you would want to change your approach.

For e.g., consider two of your cases:

Case** (i)** Element size: 0.7mm, Inflation layer total thickness: 0.3mm, Number of inflation layers: 7

Case** (ii)** Element size: 0.255mm, Inflation layer total thickness: 0.3mm, Number of inflation layers: 19

Compare the number of elements in the inflation layer and the rest of the geometry:

Case **(i)** **Inflation region**: 89,964 + **Rest of the geometry**: 24,276 = **Total**: 114,240 elements

Case **(ii)** **Inflation region**: 1,937,468 + **Rest of the geometry**: 523,587 = **Total**: 2,461,055 elements

Since its laminar flow, the total number of elements can be marginally reduced by decreasing the number of inflation layers but still performing an efficient convergence study.

Rahul

hugo CFD
posted this
21 June 2018

Hi

According to the explained I did a study for the meshes 1, 0.5, 0.25, 0.125 mm. I hit a 0.424% error for the 0.125 mesh. For the 0.25 mesh I reached a 1% error.

However, for further study, the more refined simulation takes a long time. I can use the 0.25 mesh, right?

Hugo

Kremella
posted this
21 June 2018

Hugo, Yes! 1% error is excellent. Grid independence is always a choice between maximizing accuracy and maintaining reasonable computational time. Good luck with your modeling! Best, Karthik

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